Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
Dynasoar 4
Part of Dynasoar
X-20 Dynasoar
X-20 Dynasoar at sunrise
Credit: © Mark Wade
Planned second manned Dynasoar single-orbit flight. Objectives were to demonstrate maneuver in orbit and during re-entry, and systems evaluation. Project cancelled in December 1963
Launched: 1966 Late. Number crew: 1 .
Orbital attitude maneuvers would have been made to plus/minus 90 degrees in all axes, including visual reference checks. During re-entry control maneuvers would be made at pitch angles of from 10 to 50 degrees with a 3000 m altitude margin.
Country:
USA.
Bibliography:
152,
583.
1966 Late - .
- Dynasoar 4 (cancelled) - .
Nation: USA.
Flight: Dynasoar 4.
Spacecraft: Dynasoar.
Planned date for second manned Dynasoar single-orbit flight..
Back to top of page
Home - Search - Browse - Alphabetic Index: 0- 1- 2- 3- 4- 5- 6- 7- 8- 9
A- B- C- D- E- F- G- H- I- J- K- L- M- N- O- P- Q- R- S- T- U- V- W- X- Y- Z
© 1997-2019 Mark Wade - Contact
© / Conditions for Use